Flugzeughandel - Flugzeuge zum Verkauf
Airbus Helicopter H 130 - with certified Autopilot - like new- |
[VERKAUFT] |
Übersicht
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Details
| Übersicht | |
| Typ: | Helikopter (Turbine) |
| Hersteller: | Airbus |
| Modell: | Helicopter H 130 - with certified Autopilot - like new- |
| Baujahr: | 2016 |
| RegistrierungsNr.: | D-reg |
| Eigenschaften: | Stets hangariert Gewerblich zugelassen EU-OPS 1 zugelassen |
| Standort: | Deutschland, München, EDDM |
| Gesamtzeit (TTAF): | 100 h |
| Preis: | € 3.630.000[VERKAUFT] |
| Netto-Preis: | € 3.050.000 |
| EU-versteuert: | ja |
| MwSt. ausweisbar: | ja (19%) |
| Anzahl Passagiere: | 1+4 |
| Motor(en) | |
| Anzahl Motoren: | 1 |
| Gesamtzeit: | 100 h |
| Avionik | |
|  1 avionics master switch  1 gyro-horizon  1 gyro-compass with  1 Horizontal Situation Indicator  1 turn and bank indicator  1 VHF/VOR/LOC/GS/GPS  1 transponder (mode S)  1 altitude encoder  1 Emergency Locator Transmitter  1 ICS + passenger interphone  1 VHF/VORLOC/GS Autopilot |
| Ausstattung | |
|  The EC130 T2® is certified with a pilot being on the left side  The baseline aircraft is delivered with left side controls and capabilities for the removable dual controls (copilot controls are optional)  Anti-Vibration Control System with 1 controller, actuators and accelerometers  Fuselage comprising the cabin and 3 luggage holds, with floor tie-down nets and access doors  Tail boom with stabilizer, FENESTRON® type anti torque rotor, and tail skid  Tubular skid landing gear, with replaceable skid shoes, with long footsteps (on right and on left side), profiler on rear tube, capable of taking handling wheels  Lifting points  Mooring fixtures  Single color exterior painting  Internal paint: light grey (prevailing colour)  Interior signs and markings: available in either French or English COCKPIT / CABIN  Cabin floor in light-alloy sheet-metal  1 pilot high-back energy-absorbing seat, adjustable in reach, removable, complete with cushions, safety belts and shoulder harnesses  6 passengers high-back energy-absorbing seats, removable, complete with cushions safety belts and shoulder harnesses:  2 front right, including for 1 copilot (copilot controls are optional)  4 rear row  2 cockpit jettisonable hinged doors  1 LH front door fitted with a sliding window  1 RH front door compatible with 8 seat layout  1 LH rear sliding door  1 RH rear sliding door  Locks on every access to cabin and luggage  Lock on fuel cap  Lateral and upper tinted windows (windscreen excluded)  1 ceiling housing the cabin lighting, 7 air ventilation outlets and controls (rotor brake and fuel cut-off)  Dynamic ventilation system  Cabin heating  Demisting system for front windscreens  2 pilot document holders  Door map case in LH and RH front doors  Rear bulkhead and lateral rear upholstery  1 fire-extinguisher  1 Flight Manual: available in either French or English  Interior harmony according to definition in force compartments INSTRUMENTS  1 airspeed indicator  1 altimeter  1 vertical speed indicator  1 LCD rotor and free turbine dual indicator  1 stop watch  1 warning panel  1 magnetic compass  1 heated pitot head  1 external side slip indicator  1 control box for light and electrical generation  1 ICS connection to audio warning issued from VEMD®  1 cockpit imaging and flight data monitoring device  1 LCD dual screen Vehicle and Engine Multifunction Display (VEMD) providing the following information:  First Limit Indicators (FLI)  torquemeter  exhaust gas temperature (TOT)  gas generator tachometer (N1)  Engine oil temperature, pressure  Fuel quantity  Fuel flow and estimated remaining time to fly  Ammeter and voltmeter and battery temperature  Outside Air Temperature (OAT)  Enhanced usage monitoring functions  IGE/OGE performance calculations  engine cycles counting  engine power check  overlimits display  VEMD and peripheral maintenance information  Data downloading capability (software and connection wire as option) AVIONICS  1 avionics master switch  1 gyro-horizon  1 gyro-compass with  1 Horizontal Situation Indicator  1 turn and bank indicator  1 VHF/VOR/LOC/GS/GPS  1 transponder (mode S)  1 altitude encoder  1 Emergency Locator Transmitter  1 ICS + passenger interphone  1 VHF/VORLOC/GS POWER PLANT  1 Turbomeca ARRIEL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up fuel control box that automatically controls the engine in case of a total failure of the 2 digital channels of the FADEC  1 crashworthy fuel system including 1 tank of 540 liters (143 US gal.) total capacity  1 twist grip on pilot side (for engine reduction in case of tail  1 magnetic plug and 1 chip detector  1 engine lubrication and oil cooling system  1 fire detection system  1 air-intake protection grids  1 torque-measurement pick-up rotor failure and autorotation training) TRANSMISSION SYSTEM  1 main gearbox, anti-vibration mounted, with oil sight gauge, chip detector, oil temperature and pressure switches, port for endoscope and self sealing valve for oil sampling and draining  1 main gearbox oil cooling system  1 engine to main gearbox coupling shaft  1 main rotor high and low r.p.m. warning device  1 tail drive carried by five anti-friction bearings  1 tail gearbox with oil sight gauge, chip detector and port for endoscopic inspection  1 rotor brake ROTORS AND FLIGHT CONTROLS  1 main rotor with 3 composite-material blades around a STARFLEX® head fitted with spherical thrust bearings  1 anti-torque rotor (FENESTRON) with 10 asymmetrical blades, integrated in vertical fin  3 main rotor hydraulic servo units (duplex servos)  Integrated back-up control valve on each body of each duplex servo HYDRAULIC GENERATION  2 independent hydraulic systems feeding the duplex servos ELECTRICAL INSTALLATION  One 150 A, 28 VDC starter-generator  One 15 A.h cadmium-nickel battery  1 ground power receptacle  3 position lights (LED)  1 flashing anti-collision light (LED)  2 fixed landing lights  2 cabin light sets, each with 2 reading lights for 2 rear passengers and 1 dome light  1 integrated instrument panel lighting system  Integrated lighting in central console  1 reading map light on upper canopy strut for pilot  1 cockpit breaker panel  One 28 V DC cabin power outlet AIRBORNE KIT 1  1 pitot head cover  2 static port stoppers  1 engine air-intake blanking cover  1 exhaust pipe blank  2 ground handling bogies  1 cargo net and rope  1 lifting ring  2 upper mooring rings  3 main-blade socks and pole  1 document holder  1 airborne kit stowage bag  1 front air-intake blanking cover  1 fuel tank bleeding  3 ballast plates 1 Weight not included in baseline aircraft empty weight. Appendix 2 Technical Configuration 00-10010-04-CI EC130 T2 Baseline Aircraft "as per 130 T2 15.100.03.E, and including: - VEMD - NR & NTL indicator - Control Warning Panel - Altimeter - Air Speed indicator - Vertical Speed Indicator - External side slip indicator - Stop watch - Magnetic Compass - Cockpit camera" Avionics 08-00025-03-CI VFR day and night package, included in baseline definition 06-67076-02-CI Emergency locator transmitter - Kannad INTEGRA AP-H "2 frequencies: 121.5 MHz (VHF), 406 MHz (COSPAS-SARSAT). The Programming Data Sheet must be filled and communicated by the customer two months at the latest before the helicopter's delivery." 08-11048-00-CI VHF/VOR/LOC/GS - Garmin GNC 255A 08-16119-00-CI Intercom system (ICS) - Garmin GMA 35 08-22061-01-CI Transponder (mode S) - Garmin GTX 33H The mode S identification must be communicated by the customer two months at the latest before the delivery. 08-43073-00-CI VHF/VOR/LOC/GS/GPS - Garmin GTN 750H This equipment is delivered with the original EUROPE map. Subscription for updates to be made by the customer. 08-51002-01-CI Gyro-horizon Thales H 321 EGM 08-52011-01-CI Gyro Compass Honeywell KCS 55A with Horizontal Situation Indicator Honeywell KI 525A 08-57011-01-CI Altitude encoder - Trans-cal 08-63006-01-CI Turn and Bank indicator UI 9560 - 2 - Optional Equipment List 05-02079-00-CI Engine exhaust area black thermal painting 05-21002-00-CI Cable cutter system 05-23005-00-CI Engine flushing device without removal of cowlings 05-24005-00-CI High visibility paint scheme on main rotor blades 05-25027-01-CI Enhanced Engine Air Particle Separator 05-25029-00-CI Heavy duty blade pins 05-31025-00-CI Tinted windows for front windscreens 05-31033-00-CI Sun protected upper windows 05-32012-00-CI Pilot's windshield wiper 05-37015-00-CI Dual controls 05-42025-03-CI Enhanced Air conditioning system 05-63002-03-CI Thales Avionics 200A starter-generator instead of Skurka 150A in baseline 06-11006-00-CI Short protective skid shoes 06-26026-00-CI-STC Dual external cargo sling mirrors 06-27048-00-FP Cargo sling (1500kg) - Fixed Parts 06-27048-00-RP Cargo sling (1500kg) - Removable Parts 06-42017-00-CI Landing light adjustable in site and azimuth 06-61006-00-FP Emergency floatation gear - Fixed Parts 06-93000-00-CI Additional ballast plates in tail boom Interior Layout 07-00021-02-CI STYLENCE Layout – Harmonie Scheme :Titanium Optional Avionics 08-18037-01-CI ICS installation compatible with Bose headset 08-21008-08-CI Radio altimeter Thales AHV16, instead of Turn and Bank indicator UI 9560 08-51015-01-CI Stand-by gyro-horizon Thales H321EGM 08-83017-00-CI VEMD data download kit Optional Avionics Retrofit Airbus Kassel 1 2 Axis Autopilot HeliSAS 2 Garmin G 500 H 3 Garmin TAS GTS 800 |
| Exterieur | |
| Appendix 3 Paint Scheme Exterior painting Single Colour BMW mineral grey - BMW Color Code B39 Landing gear Single Colour BMW mineral grey - BMW Color Code B39 Engine exhaust area black thermal painting |
| Stand Inspektion | |
| almost brand new on Camo Factory Warranty operated in AOC |
| Bemerkungen/Sonstiges | |
| IF THE PLANE IS SOLD WITHIN THE EU THE PURCHASE PRICE IS SUBJECT TO 19 % VAT |
Fotos
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